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ERA21LA391 · Boeing E75

30 Sept 2021 · Nicholson, PA, United States

Boeing E75 · Accident: loss of engine power (total) en route

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Event

NTSB case
ERA21LA391
Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
Accident
InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
Completed
API-reported fatalities
0 · all aircraft and ground
Ground fatalities
0
OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
General aviation
WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
Visual Meteorological Cond

Boeing E75

Aircraft type
Boeing E75
Category
Airplane
RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
N1654M
Operator
Unknown
Onboard fatalities
Unknown
Route
From not recordedTo not recorded
Aircraft age
About 78 years (built 1943)
Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
Part 91: General Aviation
Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
En route · cruise
Defining eventThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
Loss of engine power (total)
DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
Substantial

Cause areas

  • Aircraft › Aircraft power plant

Approximate · Coordinates as recorded by the NTSB; no uncertainty radius is established.

NTSB narrative

The pilot reported that, while the airplane was at an altitude of 3,500 ft, the engine lost total power. He attempted to regain engine power by adjusting the throttle, mixture control, fuel valve controls, and carburetor heat; however, the engine would not restart. As the pilot set up an approach to a nearby airstrip, he determined that the airplane would not reach the runway and performed a forced landing into trees, resulting in substantial damage to the fuselage and wings.

Postaccident examination of the engine revealed that the carburetor’s rotating mixture actuating rod was difficult to rotate, and binding occurred as the actuating rod was rotated by hand. Upon disassembly of the carburetor, the mixture control actuating rod and the metering needle, which is connected to the inner end of the rod, were found bent. No other damage to the carburetor was found. Because these components are largely or entirely internal to the carburetor, the bending of actuating rod and the metering needle was likely not a result of impact damage. The investigation was unable to determine how or when the carburetor components became bent.

Although the bends in the actuating rod and metering needle would not have prevented the mixture control from operating, the bends would have changed how the mixture setting in the carburetor responded to the mixture control lever in the cockpit. If the cockpit control was moved toward the cutoff position, the metering needle might not have performed as expected and might have moved into the cutoff position before or after the cockpit control reached its expected cutoff position. Likewise, with the cockpit control in the normal fullrich position, the metering needle might have been in a position that was either more or less than full rich. Therefore, the bent components likely resulted in a mixture setting that was not expected for any given cockpit mixture control setting. The investigation could not determine whether the mixture would have been too lean (less fuel) or too rich (more fuel), either of which could have resulted in the engine not producing power.

Four of the cylinders’ spark plugs had black-colored deposits on their electrodes, consistent with a rich mixture condition. Two spark plugs had gray-colored deposits, consistent with a normal mixture condition. The remaining three spark plugs were oil soaked, masking their electrode color, but these spark plugs would generally be more consistent with a rich mixture condition rather than a lean condition.

Probable cause

A total loss of engine power as a result of damaged internal carburetor mixture control components.

Verbatim NTSB analysis and probable cause from the NTSB dataset

Sources

NTSB record ERA21LA391
Event ID
20211005104049
Case number
ERA21LA391
Dataset
full-current
Source SHA-256
5cf380f0061817c0331a6b2d8cc7e0ee3a79bea469a1001dc5c10e56f35f5ab3
Source notes (4)
  • Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
  • Filled from the NTSB case API where the bulk record had no value: investigation status, cause areas. Values present in the bulk record are kept.
  • The date is the local date, which is the same as the UTC date the NTSB stores.
  • API snapshot SHA-256: 03b67f276003cbc54766b927bc89de6ada59e5e35beadeb050a7a700fa5ecf97; retrieved 2026-09-16T14:37:54.393Z.